Common use of New Components Clause in Contracts

New Components. i) New components should be traceable to the OEM as specified in the Type Certificate (TC) holder’s Parts Catalogue and be in a satisfactory condition for fitment. A release document issued by the OEM or Production Certificate (PC) holder should accompany the new component. The release document should clearly state that it is issued under the approval of the relevant AA under whose regulatory control the OEM or PC holder works. ii) For U.S. OEMs and PC holders release should be on the FAA Form 8130-3 as a new part. iii) For all EC States OEMs and PC holders release should be in accordance with EASA Part-21. iv) For Canadian OEMs and PC holders release should be on the Canadian; Form One as a new part. v) Standard parts are exempt from the forgoing provisions, except that such parts should be accompanied by a conformity statement and be in a satisfactory condition for fitment. vi) PMA parts may only be accepted as detailed in EASA Part-21 or in Annex 1 of the Agreement. vii) Engines rebuilt by the production approval holder can be accepted as specified in the Technical Implementation Procedures for Airworthiness and Environmental Certification (TIP- paragraph 5.1.4).

New Components. i) New components should be traceable to the OEM as specified in the Type Certificate (TC) holder’s Parts Catalogue and be in a satisfactory condition for fitmentinstallation. A release document issued by the OEM or Production Certificate (PC) holder should accompany the new component. The release document should clearly state that it is issued under the approval of the relevant AA under whose regulatory control the OEM or PC holder works. ii) For U.S. OEMs and PC holders holders, release should be on the FAA Form 8130-3 as a new part. iii) For all EC States OEMs EU Member States, OEMs, and PC holders holders, release should be in accordance with EASA Part-21Part-21 on EASA Form 1 as a new part. iv) For Canadian OEMs and PC holders release should be on the Canadian; Canadian Form One as a new part. v) Standard parts are exempt from the forgoing provisions, except that such parts should be accompanied by a conformity statement and be in a satisfactory condition for fitmentinstallation. vi) PMA parts may only be accepted as detailed in EASA Part-21 or in Annex 1 of the Agreement. vii) Engines rebuilt by the production approval holder can be accepted as specified in the Technical Implementation Procedures for Airworthiness and Environmental Certification (TIP- paragraph 5.1.4).